SA515360558B1 - نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز - Google Patents
نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغازInfo
- Publication number
- SA515360558B1 SA515360558B1 SA515360558A SA515360558A SA515360558B1 SA 515360558 B1 SA515360558 B1 SA 515360558B1 SA 515360558 A SA515360558 A SA 515360558A SA 515360558 A SA515360558 A SA 515360558A SA 515360558 B1 SA515360558 B1 SA 515360558B1
- Authority
- SA
- Saudi Arabia
- Prior art keywords
- vane carrier
- control system
- section
- cooling air
- temperature control
- Prior art date
Links
- 238000001816 cooling Methods 0.000 abstract 7
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
- F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
- F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
- F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
يتضمن نظام تحكم في درجة حرارة حامل ريشة vane carrier temperature control system يستخدم في محرك تربين يعمل بالغاز gas turbine engine مصدر هواء تبريد cooling air source أول, مصدر هواء تبريد ثاني, ونظام تحكم في درجة حرارة الهواء air temperature control system. يقوم مصدر هواء التبريد الأول بإمداد جزء أول من هواء تبريد حامل ريشة تم استخراجه من قطاع ضاغط compressor للمحرك engine إلى قطاع أول لحامل ريشة vane carrier يحمل عديد من صفوف أرياش داخل قطاع تربين للمحرك. يقوم مصدر هواء التبريد الثاني بإمداد جزء ثاني من هواء تبريد حامل ريشة مستخرج من قطاع الضاغط إلى قطاع ثاني لحامل الريشة المباعد عن القطاع الأول في اتجاه محوري محدد باتجاه تدفق غاز التشغيل الساخن hot working gas flow من خلال قطاع التربين. يقوم نظام التحكم في درجة حرارة الهواء بالتحكم في درجة حرارة واحد على الأقل من أجزاء هواء تبريد حامل الريشة الأولى والثانية. شكل 1
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/719,269 US9562475B2 (en) | 2012-12-19 | 2012-12-19 | Vane carrier temperature control system in a gas turbine engine |
PCT/US2013/076099 WO2014100164A1 (en) | 2012-12-19 | 2013-12-18 | Vane carrier temperature control system in a gas turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
SA515360558B1 true SA515360558B1 (ar) | 2018-09-24 |
Family
ID=49917293
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SA515360558A SA515360558B1 (ar) | 2012-12-19 | 2015-06-10 | نظام للتحكم في درجة حرارة حامل ريشة في محرك تربين يعمل بالغاز |
Country Status (7)
Country | Link |
---|---|
US (1) | US9562475B2 (ar) |
EP (1) | EP2935831A1 (ar) |
JP (1) | JP6165879B2 (ar) |
CN (1) | CN104884767B (ar) |
RU (1) | RU2626923C2 (ar) |
SA (1) | SA515360558B1 (ar) |
WO (1) | WO2014100164A1 (ar) |
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US10830148B2 (en) | 2015-04-24 | 2020-11-10 | Raytheon Technologies Corporation | Intercooled cooling air with dual pass heat exchanger |
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US10794288B2 (en) | 2015-07-07 | 2020-10-06 | Raytheon Technologies Corporation | Cooled cooling air system for a turbofan engine |
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US10669940B2 (en) | 2016-09-19 | 2020-06-02 | Raytheon Technologies Corporation | Gas turbine engine with intercooled cooling air and turbine drive |
US10794290B2 (en) | 2016-11-08 | 2020-10-06 | Raytheon Technologies Corporation | Intercooled cooled cooling integrated air cycle machine |
US20180128187A1 (en) * | 2016-11-08 | 2018-05-10 | United Technologies Corporation | Cooled cooling air safety through a temperature-monitoring line replaceable unit |
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JP6799455B2 (ja) * | 2016-12-16 | 2020-12-16 | 川崎重工業株式会社 | ガスタービンエンジン |
US10961911B2 (en) | 2017-01-17 | 2021-03-30 | Raytheon Technologies Corporation | Injection cooled cooling air system for a gas turbine engine |
US10995673B2 (en) | 2017-01-19 | 2021-05-04 | Raytheon Technologies Corporation | Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox |
EP3379036B1 (en) * | 2017-03-22 | 2024-09-04 | Ansaldo Energia Switzerland AG | Gas turbine engine |
CN106801646A (zh) * | 2017-03-23 | 2017-06-06 | 重庆大学 | 一种新型燃气轮机及提高燃气透平进口温度的方法 |
US10577964B2 (en) | 2017-03-31 | 2020-03-03 | United Technologies Corporation | Cooled cooling air for blade air seal through outer chamber |
US10711640B2 (en) | 2017-04-11 | 2020-07-14 | Raytheon Technologies Corporation | Cooled cooling air to blade outer air seal passing through a static vane |
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US10641121B2 (en) * | 2017-07-24 | 2020-05-05 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with rotor tip clearance control system |
DE102017216119A1 (de) * | 2017-09-13 | 2019-03-14 | MTU Aero Engines AG | Gasturbinenverdichtergehäuse |
US10738703B2 (en) | 2018-03-22 | 2020-08-11 | Raytheon Technologies Corporation | Intercooled cooling air with combined features |
KR102067103B1 (ko) * | 2018-04-05 | 2020-01-16 | 두산중공업 주식회사 | 터빈의 온도 추정 시스템 |
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-
2012
- 2012-12-19 US US13/719,269 patent/US9562475B2/en not_active Expired - Fee Related
-
2013
- 2013-12-18 WO PCT/US2013/076099 patent/WO2014100164A1/en active Application Filing
- 2013-12-18 CN CN201380066466.5A patent/CN104884767B/zh not_active Expired - Fee Related
- 2013-12-18 EP EP13815933.0A patent/EP2935831A1/en not_active Withdrawn
- 2013-12-18 JP JP2015549620A patent/JP6165879B2/ja not_active Expired - Fee Related
- 2013-12-18 RU RU2015129105A patent/RU2626923C2/ru not_active IP Right Cessation
-
2015
- 2015-06-10 SA SA515360558A patent/SA515360558B1/ar unknown
Also Published As
Publication number | Publication date |
---|---|
US9562475B2 (en) | 2017-02-07 |
CN104884767B (zh) | 2018-03-23 |
RU2015129105A (ru) | 2017-01-25 |
EP2935831A1 (en) | 2015-10-28 |
CN104884767A (zh) | 2015-09-02 |
RU2626923C2 (ru) | 2017-08-02 |
US20140311157A1 (en) | 2014-10-23 |
WO2014100164A1 (en) | 2014-06-26 |
JP2016503855A (ja) | 2016-02-08 |
JP6165879B2 (ja) | 2017-07-19 |
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